Braking torque control system
AssigneeThe Boeing Company
InventorsRobert L. Amberg, Andrew M. Valaas
Life of this patent
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AssigneeThe Boeing Company
InventorsRobert L. Amberg, Andrew M. Valaas
Estimating the term…
A system for controlling the torque developed by a fluid actuated brake as it slows an aircraft wheel. In one embodiment, the system includes a strain gauge (62) for sensing the load applied to a brake metering valve (16). In another embodiment, the pressure of the hydraulic fluid output from the brake metering valve is sensed by a pressure transducer (42). Depending upon the sensor used, the system is operative to control the pressure applied to a brake assembly (54) of an aircraft as a function of the mechanical load or pressure. The system includes a torque control (50,120) connected to control one or more valves (22, or 83 and 102), modulating the pressure of hydraulic fluid applied to the brake assembly; the valves may be part of an antiskid control system. A torque sensor (46) is disposed on a torque reaction arm (36) and produces a signal indicative of the torque developed by the brake assembly. The torque control reduces the pressure of the hydraulic fluid applied to the brake assembly if the torque produced by the brake exceeds a value determined as a function of the magnitude of the force applied to actuate the brake.
A system for controlling a torque developed by a fluid pressure activated brake as it slows a rolling wheel, comprising:
A system for controlling a torque developed by a fluid pressure actuated brake as it slows a rolling wheel that is adapted to operate in parallel with an antiskid brake control system, comprising:
A system for controlling a torque developed by a fluid pressure actuated brake applied to slow a rolling wheel, the system comprising:
A method for controlling a torque developed by a fluid pressure actuated brake as it slows a rolling wheel, comprising the steps of:
Dependencies are inferred from the claim text.